Garmin G1000 - Piper PA-34-220T Seneca User guide

260

250

240

210

200

190

225

12000

18000

11900

11700

11600

11800

TAS 269

KT

29.86

IN

2

1

2

10 10

10

E

S

W

N

3

6

12

15

21

24

30

33

500

360‘

GPS ENR

l0

20

l0

29.9

29.8

1

2

3

4

5

6

7

8

9

100 FEET

In Hg

ALT

NO PITCH

INFORMATION

D.C.

ELEC.

TURN COORDINATOR

2 MIN.

R

L

10

UP

DOWN

VERTICAL SPEED

100 FEET PER MINUTE

15

155

5

10

20

0

Garmin International, Inc.

1200 East 151st Street

Olathe, KS 66062, U.S.A.

p:913.397.8200 f:913.397.8282

Garmin AT, Inc.

2345 Turner Road SE

Salem, OR 97302, U.S.A.

p:503.391.3411 f:503.364.2138

Garmin (Europe) Ltd.

Liberty House,

Hounsdown Business Park

Southampton, Hampshire

SO40 9LR U.K.

p:44 (0) 23 8052 4000

f:44 (0) 23 8052 4004

Aviation Support:44 (0) 87 0850 1243

Garmin Corporation

No. 68, Jangshu 2nd Road

Shijr, Taipei County, Taiwan

p:886/02.2642.9199

f:886/02.2642.9099

www.garmin.com

G1000

®

Pilot’s Guide

Piper PA-34-220T

Seneca

190-01404-01

Revision B

PILOT’S GUIDEPILOT’S GUIDE

Piper PA-34-220T Seneca

G1000

®

Integrated Avionic System

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

ENGINE INDICATION SYSTEM

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AUTOMATIC FLIGHT CONTROL SYSTEM

ADDITIONAL FEATURES

APPENDICES

INDEX

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. B

This manual reﬂects the operation of System Software version 1981.01 or later. Some differences in operation may be observed when

comparing the information in this manual to earlier or later software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.

Tel: 913/397.8200 Fax: 913/397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.

Tel: 503/391.3411 Fax: 503/364.2138

Garmin (Europe) Ltd., Liberty House, Hounsdown Business Park, Southampton, SO40 9LR, U.K

Tel: 44 (0) 23 8052 4000 Fax: 44 (0) 23 8052 4004 Aviation Support:44 (0) 87 0850 1243

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan

Tel: 886/02.2642.9199 Fax: 886/02.2642.9099

For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please

contact Garmin’s AOG Hotline at 913.397.0836.

Website Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored

in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download

a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for

personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice

and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin

®

and G1000

®

are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts

®

, SafeTaxi

®

, and Garmin ESP

™

are trademarks

of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.; SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite

Radio, Inc.

AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties,

with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties

of merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any

representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any

incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if

AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to

the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual

or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for

incidental or consequential damages so the above limitations or exclusions may not apply to you.

AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with

respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of

merchantability and ﬁtness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or

make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the

maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related

to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions

do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations

or exclusions may not apply to licensee.

June 2014 Printed in the U.S.A

190-01404-01 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

i

WARNINGS, CAUTIONS, AND NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance

feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance

and does not relieve the pilot from the responsibility of being aware of surroundings during ﬂight. The

terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from

third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be

relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current

aeronautical charts for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and

could vary signiﬁcantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data

Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always

use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated

regularly in order to ensure that the information remains current. Pilots using any outdated database do so

entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is

intended only to supplement other approved navigation data sources and should be considered as an aid to

enhance situational awareness.

WARNING: Do not rely solely upon the display of trafﬁc information for collision avoidance maneuvering.

The trafﬁc display does not provide collision avoidance resolution advisories and does not under any

circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft.

WARNING: Do not rely solely upon the display of trafﬁc information to accurately depict all of the trafﬁc

within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information

from aircraft or ground stations, trafﬁc may be present that is not represented on the display.

WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous

weather avoidance. Range limitations and interference may cause the system to display inaccurate or

incomplete information. Refer to documentation from the lightning detection system manufacturer for

detailed information about the system.

WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous

weather. Information contained within data link weather products may not accurately depict current

weather conditions.

WARNING: Do not use the indicated data link weather product age to determine the age of the weather

information shown by the data link weather product. Due to time delays inherent in gathering and processing

weather data for data link transmission, the weather information shown by the data link weather product

may be signiﬁcantly older than the indicated weather product age.

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. Bii

WARNINGS, CAUTIONS, AND NOTES

WARNING:

For safety reasons, G1000 operational procedures must be learned on the ground.

WARNING:

The Garmin G1000, as installed in this aircraft, has a very high degree of functional integrity.

However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable

system failures is not practical.

WARNING:

The United States government operates the Global Positioning System and is solely responsible

for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy

and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic

NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be

misused or misinterpreted and, therefore, become unsafe.

WARNING:

To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000

Pilot’s Guide documentation and the G1000 Integrated Avionics System in the Airplane Flight Manual.

Thoroughly practice basic operation prior to actual use. During ﬂight operations, carefully compare indications

from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual

sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.

WARNING: Do not use the system to attempt to penetrate a thunderstorm. The illustrations in this guide are

only examples. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information

Manual (AIM) recommend avoiding any thunderstorm identiﬁed as severe of giving intense radar echo by

at least 20 miles.

WARNING

:

Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of

according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/

aboutGarmin/environment/disposal.jsp.

WARNING

:

Because of variation in the earth’s magnetic ﬁeld, operating the G1000 within the following

areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all

longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between longitude

75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and 128° W.

(Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia);

South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New

Zealand)

WARNING

:

Do not use GPS to navigate to any active waypoint identiﬁed as a ‘NON WGS84 WPT’ by a

system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that

may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned

in error as displayed.

190-01404-01 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

iii

WARNINGS, CAUTIONS, AND NOTES

CAUTION: The PFD and MFD displays use a lens coated with a special anti-reﬂective coating that is very

sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE

ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an

eyeglass lens cleaner that is speciﬁed as safe for anti-reﬂective coatings.

CAUTION:

The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by

an authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty

and the pilot’s authority to operate this device under FAA/FCC regulations.

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby

thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of

two or more discharge points in the strike display mode do indicate thunderstorm activity if these points

reappear after the screen has been cleared.

NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.

Always conﬁrm TFR information through ofﬁcial sources such as Flight Service Stations or Air Trafﬁc Control.

NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and

displays, are subject to change and may not reﬂect the most current G1000 system and aviation databases.

Depictions of equipment may differ slightly from the actual equipment.

NOTE

: This device complies with part 15 of the FCC Rules. Operation is subject to the following two

conditions: (1) this device may not cause harmful interference, and (2) this device must accept any

interference received, including interference that may cause undesired operation.

NOTE

: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of

attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards

away from the source of the interference should alleviate the condition.

NOTE

: Use of polarized eyewear may cause the ﬂight displays to appear dim or blank.

NOTE

: This product, its packaging, and its components contain chemicals known to the State of California

to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with

California’s Proposition 65. If you have any questions or would like additional information, please refer to

our web site at www.garmin.com/prop65.

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. Biv

WARNINGS, CAUTIONS, AND NOTES

NOTE

: The FAA has asked Garmin to remind pilots who ﬂy with Garmin database-dependent avionics of the

following:

• It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information

related to the use of databases in the National Airspace System.

• Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases

obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue

of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database

and can be viewed at http://ﬂy.garmin.com by selecting ‘Type 2 LOA Status.’

• Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with

established FAA regulatory guidance, but does not constitute authorization to ﬂy any and all terminal procedures

that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established

AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment.

NOTE

: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed

in SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at

www.ﬂygarmin.com by selecting ‘Database Exclusions List.’

NOTE

: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their

impact on the intended aircraft operation. The database alerts can be viewed at www.ﬂygarmin.com by

selecting ‘Aviation Database Alerts.’

NOTE

: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to

coordinate the revised DQRs.

NOTE: Garmin requests the ﬂight crew report any observed discrepancies related to database information.

These discrepancies could come in the form of an incorrect procedure; incorrectly identiﬁed terrain, obstacles

and ﬁxes; or any other displayed item used for navigation or communication in the air or on the ground. Go

to FlyGarmin.com and select ‘Report An Aviation Data Error Report.’

190-01404-01 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

v

REVISION INFORMATION

Record of Revisions

Part Number Revision Date Page Range Description

190-01404-00 A 5/22/13 i – I-6 Initial release

190-01404-01 A 3/20/14 i – I-6 Added Garmin AFCS

Added Becker ADF

190-01404-01 B 6/30/14 i – I-6 Removed USP

Added Pitch Trim in Motion message

Updated System Software number

Added database notes

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. Bvi

TABLE OF CONTENTS

SECTION 1 SYSTEM OVERVIEW

1.1 Line Replaceable Units ........................................... 2

1.2 Secure Digital (SD) Cards .......................................6

1.3 System Power-up ..................................................... 7

1.4 System Operation .................................................... 8

Display Operation ......................................................... 8

G1000 System Annunciations ........................................ 9

System Status ............................................................. 10

AHRS Operation ......................................................... 12

GPS Receiver Operation .............................................. 13

1.5 G1000 Controls ...................................................... 18

PFD/MFD Controls ...................................................... 18

Additional MFD Controls (Garmin AFCS Installed) .......... 20

Softkey Function ......................................................... 21

1.6 Accessing G1000 Functionality............................ 29

Menus ....................................................................... 29

Data Entry.................................................................. 29

Page Groups .............................................................. 31

System Settings .......................................................... 35

System Utilities ........................................................... 45

1.7 Display Backlighting ............................................. 49

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments ................................................. 54

Airspeed Indicator ...................................................... 54

Attitude Indicator ....................................................... 56

Altimeter ................................................................... 57

Vertical Speed Indicator (VSI) ....................................... 61

Vertical Deviation ....................................................... 61

Horizontal Situation Indicator (HSI) .............................. 62

Course Deviation Indicator (CDI) .................................. 67

2.2 Supplemental Flight Data .................................... 75

Temperature Displays .................................................. 75

Wind Data ................................................................. 76

Vertical Navigation (VNV) Indications ........................... 77

2.3 PFD Annunciations and Alerting Functions ........ 78

System Annunciations ................................................. 78

Marker Beacon Annunciations...................................... 79

Trafﬁc Annunciation .................................................... 79

TAWS Annunciations ................................................... 80

Altitude Alerting ......................................................... 80

Low Altitude Annunciation .......................................... 81

Minimum Descent Altitude/Decision Height Alerting ...... 81

2.4 Abnormal Operations ........................................... 83

Abnormal GPS Conditions ........................................... 83

Unusual Attitudes ....................................................... 84

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

3.1 Engine Display ....................................................... 86

3.2 Engine Page............................................................ 88

Electrical .................................................................... 90

Cylinder Head Temperatures ........................................ 90

Fuel Calculations ........................................................ 91

Oil Pressure and Temperature Gauges ........................... 93

Systems ..................................................................... 93

Fuel Quantity ............................................................. 94

Flap Indications .......................................................... 94

Landing Gear Indications ............................................. 95

EIS Display (Reversionary Mode) .................................. 96

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview ................................................................ 97

PFD Controls and Frequency Display ............................. 98

GMA 1347 Audio Panel Controls ................................ 100

4.2 COM Operation .................................................... 102

COM Transceiver Selection and Activation ................... 102

COM Transceiver Manual Tuning ................................ 103

Quick-tuning and Activating 121.500 MHz .................. 104

Auto-tuning the COM Frequency ................................ 105

Auto-tuning from the MFD ........................................ 106

Frequency Spacing .................................................... 109

Automatic Squelch .................................................... 110

Volume .................................................................... 110

4.3 NAV Operation ..................................................... 111

NAV Radio Selection and Activation ........................... 111

NAV Receiver Manual Tuning ..................................... 112

Auto-tuning a NAV Frequency from the MFD ............... 114

Auto-tuning NAV Frequencies on Approach Activation . 118

Marker Beacon Receiver ............................................ 119

ADF/DME Tuning (Optional) ....................................... 120

4.4 GTX 33 Mode S Transponder .............................. 124

Transponder Controls ................................................ 124

Transponder Mode Selection ...................................... 125

190-01404-01 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

vii

TABLE OF CONTENTS

Entering a Transponder Code ..................................... 127

IDENT Function ........................................................ 128

Flight ID Reporting.................................................... 129

4.5 Additional Audio Panel Functions ..................... 130

Power-Up ................................................................. 130

Mono/Stereo Headsets .............................................. 130

Speaker ................................................................... 130

Intercom .................................................................. 131

Passenger Address (PA) System .................................. 133

Clearance Recorder and Player ................................... 133

Split COM Operation ................................................. 134

Entertainment Inputs ................................................ 135

4.6 Audio Panel Preﬂight Procedure ....................... 136

4.7 Abnormal Operation ........................................... 137

Stuck Microphone ..................................................... 137

COM Tuning Failure ................................................... 137

Audio Panel Fail-safe Operation .................................137

PFD Failure (Reversionary Mode) ............................... 137

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 139

Navigation Status Box ............................................... 140

5.2 Using Map Displays ............................................. 142

Map Orientation ....................................................... 142

Map Range .............................................................. 144

Map Panning ............................................................ 146

Measuring Bearing and Distance ................................ 150

Topography .............................................................. 151

Map Symbols ........................................................... 154

Airways ................................................................... 160

Track Vector ............................................................. 162

Wind Vector ............................................................. 163

Nav Range Ring........................................................ 164

Fuel Range Ring ....................................................... 165

Field of View (SVS) .................................................... 166

Selected Altitude Intercept Arc ................................... 167

5.3 Waypoints ............................................................. 168

Airports ................................................................... 169

Intersections ............................................................ 176

NDBs ....................................................................... 178

VORs ....................................................................... 180

User Waypoints ........................................................ 182

5.4 Airspaces .............................................................. 188

5.5 Direct-to-Navigation .......................................... 192

5.6 Flight Planning ..................................................... 198

Flight Plan Creation .................................................. 199

Adding Waypoints to an Existing Flight Plan ................ 204

Adding Airways to a Flight Plan ................................. 206

Adding Procedures to a Stored Flight Plan .................. 209

Flight Plan Storage ................................................... 216

Flight Plan Editing .................................................... 218

Along Track Offsets ................................................... 221

Parallel Track ............................................................ 223

Activating a Flight Plan Leg ....................................... 226

Inverting a Flight Plan ............................................... 227

Flight Plan Views ...................................................... 228

Closest Point of FPL .................................................. 230

User-Deﬁned Holding Patterns ................................... 230

5.7 Vertical Navigation ............................................. 235

Altitude Constraints .................................................. 237

5.8 Procedures ...........................................................241

Departures ............................................................... 241

Arrivals ................................................................... 244

Approaches ............................................................. 246

5.9 Trip Planning ........................................................ 254

Trip Planning ............................................................ 254

5.10 RAIM Prediction................................................... 258

5.11 Navigating a Flight Plan ..................................... 262

5.12 Abnormal Operation ........................................... 290

SECTION 6 HAZARD AVOIDANCE

6.1 SiriusXM Weather ................................................ 294

Activating Services .................................................... 294

Using SiriusXM Weather Products .............................. 295

SiriusXM Weather Abnormal Operations ..................... 329

6.2 Garmin Connext Weather ................................... 331

Registering the Iridium Satellite System ...................... 331

Registering Garmin Connext Weather ......................... 332

Accessing Garmin Connext Weather Products .............. 333

Connext Data Requests ............................................. 341

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. Bviii

TABLE OF CONTENTS

Garmin Connext Weather Products ............................. 345

Abnormal Operations ................................................ 361

6.3 Airborne Color Weather Radar .......................... 363

System Description ................................................... 363

Principles of Pulsed Airborne Weather Radar ............... 363

Safe Operating Distance ............................................ 367

Basic Antenna Tilt Setup ............................................ 368

Weather Mapping and Interpretation ......................... 369

Ground Mapping and Interpretation ........................... 380

System Status ........................................................... 381

6.4 Stormscope Lightning ......................................... 382

Setting Up Stormscope on the Navigation Map ........... 382

Selecting the Stormscope Page .................................. 386

6.5 Terrain Proximity ................................................. 387

Displaying Terrain Proximity Data ............................... 387

6.6 Proﬁle View Terrain ............................................. 392

Proﬁle View Display .................................................. 393

6.7 Terrain-SVS ........................................................... 396

Displaying Terrain-SVS Data ....................................... 397

Terrain-SVS Page ...................................................... 399

Terrain-SVS Alerts ..................................................... 401

System Status ........................................................... 404

6.8 TAWS-B ................................................................. 405

Displaying TAWS-B Data ............................................ 406

TAWS-B Page ........................................................... 409

TAWS-B Alerts .......................................................... 411

System Status ........................................................... 417

6.9 Trafﬁc Information Service (TIS) ........................ 419

Displaying TRAFFIC Data ........................................... 420

Trafﬁc Map Page ....................................................... 422

TIS Alerts ................................................................. 423

System Status ........................................................... 424

6.10 GTS 825 Trafﬁc ..................................................... 427

Theory of operation .................................................. 427

TAS Alerts ................................................................ 430

System Test .............................................................. 431

Operation ................................................................ 432

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 Basic Autopilot Operation .................................. 442

7.2 AFCS Controls ...................................................... 443

7.3 Flight Director Operation ................................... 445

Activating the Flight Director ..................................... 445

AFCS Status Box ....................................................... 446

Flight Director Modes ................................................ 447

Command Bars ......................................................... 447

7.4 Vertical Modes ..................................................... 448

Pitch Hold Mode (PIT) ............................................... 449

Selected Altitude Capture Mode (ALTS) ....................... 450

Altitude Hold Mode (ALT) .......................................... 451

Vertical Speed Mode (VS) .......................................... 452

Flight Level Change Mode (FLC) ................................. 453

Vertical Navigation Modes (VPTH, ALTV) ..................... 454

Glidepath Mode (GP) ................................................ 458

Glideslope Mode (GS) ............................................... 460

Takeoff (TO) and Go Around (GA) Modes .................... 461

7.5 Lateral Modes ...................................................... 462

Roll Hold Mode (ROL) ............................................... 463

Heading Select Mode (HDG) ...................................... 464

Navigation Modes (GPS, VOR, LOC, BC) ...................... 465

Approach Modes (GPS, VAPP, LOC) ............................. 467

7.6 Autopilot and Yaw Damper Operation ............. 469

Flight Control ........................................................... 469

Engagement ............................................................. 470

Control Wheel Steering ............................................. 470

Disengagement ........................................................ 471

Level Mode .............................................................. 472

7.7 Example Flight Plan ............................................ 473

Departure ................................................................ 473

Intercepting a VOR Radial .......................................... 475

Flying a Flight Plan/GPS Course ................................. 476

Descent ................................................................... 476

Approach ................................................................. 480

Go Around/Missed Approach ..................................... 484

190-01404-01 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

ix

TABLE OF CONTENTS

7.8 AFCS Annunciations and Alerts ......................... 486

AFCS Status Alerts .................................................... 486

Overspeed Protection ................................................ 487

7.9 Abnormal Operation ........................................... 488

Suspected Autopilot Malfunction ............................... 488

Overpowering Autopilot Servos .................................. 488

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision Technology (SVT) ..................... 490

SVT Operation .......................................................... 491

SVT Features ............................................................ 493

Field of View ............................................................ 502

8.2 SafeTaxi ................................................................ 504

SafeTaxi Cycle Number and Revision .......................... 507

8.3 ChartView ............................................................. 510

ChartView Softkeys ................................................... 511

Terminal Procedures Charts ....................................... 512

Chart Options ........................................................... 520

Day/Night View ........................................................ 526

ChartView Cycle Number and Expiration Date ............. 528

8.4 FliteCharts ............................................................ 531

FliteCharts Softkeys .................................................. 532

Terminal Procedures Charts ....................................... 533

Chart Options ........................................................... 540

Day/Night View ........................................................ 544

FliteCharts Cycle Number and Expiration Date ............. 546

8.5 Airport Directory ................................................. 549

Airport Directory Database Cycle Number and Revision 550

8.6 Satellite Telephone Services .............................. 552

Registering the System .............................................. 552

Telephone Communication ........................................ 552

Text Messaging (SMS) ............................................... 558

8.7 SiriusXM Satellite Radio Entertainment ........... 570

Activating SiriusXM Satellite Radio Services ................ 570

Using SiriusXM Radio ................................................ 572

8.8 Scheduler .............................................................. 575

8.9 Flight Data Logging ............................................ 577

8.10 Electronic Stability & Protection (ESP

™

) ........... 579

Roll Engagement ...................................................... 580

Pitch Engagement..................................................... 582

High Airspeed Protection ........................................... 582

8.11 Abnormal Operation ........................................... 583

SVT Troubleshooting ................................................. 583

Reversionary Mode ................................................... 583

Unusual Attitudes ..................................................... 584

APPENDICES

Annunciations and Alerts ............................................. 587

CAS Messages .......................................................... 589

System Messages ..................................................... 590

Comparator Annunciations ........................................ 590

Reversionary Sensor Annunciations ............................ 591

Miscellaneous Annunciations ..................................... 591

G1000 System Message Advisories ............................. 594

Voice Alerts .............................................................. 606

AFCS Alerts .............................................................. 607

Terrain-SVS Alerts ..................................................... 608

Terrain-SVS System Status Annunciations .................... 608

TAWS-B ALERTS ........................................................ 609

TAWS-B System Status Annunciations ......................... 610

Flight Plan Import/Export Messages ........................... 610

Pilot Proﬁle Import/Export Messages .......................... 611

Database Management ................................................ 613

Navigation Databases ............................................... 614

Garmin Databases .................................................... 618

Garmin Aviation Glossary ............................................ 625

Frequently Asked Questions ........................................ 633

General TIS Information ............................................... 637

Map Symbols ................................................................. 639

INDEX

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. Bx

TABLE OF CONTENTS

Blank Page

190-01404-01 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

1

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

SECTION 1 SYSTEM OVERVIEW

The G1000 Integrated Avionics System presents ﬂight instrumentation, position, navigation, communication,

and identiﬁcation information to the pilot using ﬂat-panel color displays. The system is distributed across the

following Line Replaceable Units (LRUs):

•

GDU 1040

Primary Flight Display (PFD)

•

GDU 1040

Multi Function Display (MFD)

•

GMA 1347

Audio Panel with Integrated Marker Beacon Receiver

•

GIA 63W

Integrated Avionics Unit (IAU)

•

GDC 74A

Air Data Computer (ADC)

•

GEA 71

Engine/Airframe Unit

•

GTX 33

Mode S Transponder

•

GRS 77

Attitude and Heading Reference System (AHRS)

•

GMU 44

Magnetometer

The G1000 is capable of interfacing with the following optional equipment:

•

GDL 69A

Data Link Receiver

•

GWX 68

Weather Radar

•

GTS 825

Trafﬁc Advisory System

•

GSR 56

Iridium Transceiver

•

GDU 1044/1045

Multi Function Display (MFD)

•

GSA 80

AFCS Servos

•

GSM 86

Servo Gearboxes

KN 63 DME

KR 87 ADF

Becker ADF

WX-500 Stormscope

Figure 1-1 shows interactions between the LRUs.

The Garmin Automated Flight Control System (AFCS) provides the ﬂight director (FD) and autopilot (AP)

functions of the G1000 system.

NOTE: Refer to the AFCS section for details on the Garmin AFCS.

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. B2

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

1.1 LINE REPLACEABLE UNITS

• GDU 1040 (2) – The left and right GDUs are conﬁgured as Primary Flight Displays (PFDs). Both feature 10.4-

inch LCD screens with 1024 x 768 resolution. The displays communicate with each other through a High-

Speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an Ethernet connection to an

IAU.

• GDU 1040/1044/1045 (1) – The middle GDU is conﬁgured as a Multi Function Display (MFD). It features

a 10.4-inch LCD screens with 1024 x 768 resolution. The displays communicate with each other through a

High-Speed Data Bus (HSDB) Ethernet connection. Either the GDU 1044 or the GDU 1045 is used when the

Garmin AFCS is installed.

•

GMA 1347

(1) – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio,

intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual

control of display reversionary mode (red

DISPLAY BACKUP

Button; see Section 1.5, System Operation) and

communicates with both IAUs using an RS-232 digital interface.

• GIA 63W (2) – The Integrated Avionics Units (IAU) function as the main communication hubs, linking all

LRUs with the on-side display. Each IAU contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, and

system integration microprocessors, and is paired with the on-side display via HSDB connection. The IAUs are

not paired together and do not communicate with each other directly.

190-01404-01 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

3

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

•

GDC 74A (1 or 2)

– The Air Data Computer (ADC) processes data from the pitot/static system and outside air

temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information

to the system. It communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface.

•

GEA 71

(2) – The Engine Airframe Units receive and process signals from the engine and airframe sensors.

These units communicates with both IAUs using an RS-485 digital interface.

•

GTX 33 (1)

– The solid-state Transponder provides Modes A, C, and S capability and communicates with both

IAUs through an RS-232 digital interface.

•

GRS 77 (1 or 2)

– The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading

information via ARINC 429 to both PFDs and the primary IAU. The AHRS contains advanced sensors (including

accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic ﬁeld information,

with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation is discussed

in Section 1.4, System Operation.

•

GMU 44 (1 or 2)

– The Magnetometer measures local magnetic ﬁeld and sends data to the AHRS for processing

to determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates

with it via an RS-485 digital interface.

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. B4

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

•

GDL 69A

(1 optional) – The Data Link Satellite Radio Receiver provides real-time weather information to the

G1000 MFD and PFD Inset Map, as well as digital audio entertainment. The Data Link Receiver communicates

with the MFD via a HSDB connection. A subscription to SiriusXM Satellite Radio Service is required to enable

the GDL 69A capability.

•

GWX 68

(1 optional) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL

69A (or directly to the MFD without a GDL 69A), via HSDB connection.

•

GTS 825

(1 optional) – The GTS 825 provides real-time trafﬁc information to the MFD (and, indirectly, to the

inset map of the PFD). The GTS 825 communicates with the MFD with an HSDB connection.

•

GSR 56

(1 optional) – The Iridium Transceiver provides voice communication by means of pilot and copilot

headsets. The unit can also send and receive data over the Iridium satellite network. The GSR 56 is connected

to the #2 GIA 63W with an RS-232 digital interface.

•

GSA 80

(4) (only with Garmin AFCS option) – The GSA 80 servos are used for the automatic control of pitch

and yaw. These units interface with each GIA 63W.

The GSM 86 servo gearboxes are responsible for transferring the output torque of the GSA 80 servo actuators

to the mechanical ﬂight-control surface linkage.

190-01404-01 Rev. B

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

5

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICES INDEX

#1

GDU 1040

(PFD1)

GSR 56

(Iridium)

GDL 69A

(XM Weather/

Audio Datalink)

GMA 1347

(Audio

Panel)

KN-63

(DME)

#1 GIA 63W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

Flight

Director

AFCS Mode

Logic

Servo Logic

#2 GIA 63W

(Integrated

Avionics

Unit)

VHF COM

GPS/SBAS

VOR/LOC

G/S

Flight

Director

AFCS Mode

Logic

Servo Logic

#2

GDU 1040

(PFD2)

Non-Garmin Equipment

KR-87 or

Becker

(ADF)

WX-500

(Stormscope)

GTX 33

(Transponder)

#3

GDU 1040

(MFD)

or

GDU 1044

(MFD)

or

GDU 1045

(MFD)

#1 GEA 71 (Engine

& Airframe I/F)

#1 GDC 74A

(Air Data

Computer)

#2 GDC 74A

(Air Data

Computer)

#1 GRS 77

(Attitude &

Heading)

#2 GRS 77

(Attitude &

Heading)

Optional

Garmin Equipment

Optional

Non-Garmin Equipment

GSA 80 (4)

(Garmin AFCS

Servos)

GWX 68

(Weather

Radar)

#1 GMA 44

(Magnetometer)

#2 GMA 44

(Magnetometer)

#2 GEA 71 (Engine

& Airframe I/F)

GTS 825

(TAS)

Garmin Equipment

Figure 1-1 System Block Diagram

NOTE: For information on non-Garmin optional/additional equipment shown in Figure 1-1, consult the

applicable optional interface user’s guide. This document assumes that the reader is already familiar with

the operation of this additional equipment.

Garmin G1000 Pilot’s Guide for the Piper PA-34-220T Seneca

190-01404-01 Rev. B6

SYSTEM OVERVIEW

SYSTEM

OVERVIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO PANEL

& CNS

FLIGHT

MANAGEMENT

HAZARD

AVOIDANCE

AFCS

ADDITIONAL

FEATURES

APPENDICESINDEX

1.2 SECURE DIGITAL (SD) CARDS

NOTE:

Ensure the G1000 System is powered off before inserting an SD card.

NOTE:

Refer to Appendix B for instructions on updating the aviation database.

The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the

display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database

and system software updates, terrain database storage, and to provide for the import or export of data including

ﬂight plans, pilot proﬁles, and ﬂight data logs.

Installing an SD card:

1) Insert the SD card in the SD card slot (the front of the card should be ﬂush with the face of the display bezel).

2) To eject the card, gently press on the SD card to release the spring latch.

Figure 1-2 Display Bezel SD Card Slots

SD Card Slots

Page is loading ...

Garmin G1000 - Piper PA-34-220T Seneca, G1000: Piper PA-34-220T Seneca User guide

Related papers

Other documents